基于自适应观测器和自抗扰控制的PMSM直接转矩控制

提出一种新的自适应观测器,用于永磁同步电机直接转矩控制系统的定子磁链和定子电阻估计。该观测器利用静止坐标系下的电压模型估计定子磁链,采用转子坐标系下的电流模型估计定子电流,把定子电流估计误差通过增益矩阵作为反馈信号。定子电阻自适应律根据李亚普诺夫稳定性理论推出,观测器的增益矩阵采用极点配置方法得到,观测器的收敛性根据李亚普诺夫稳定性分析来保证。此外,采用自抗扰控制技术设计了速度控制器,该控制器能对负载扰动进行估计和补偿。仿真结果证明了所提自适应观测器的有效性和自抗扰控制器的抗负载扰动能力。

Abstract：

A new adaptive observer was proposed to estimate the stator flux and stator resistance in the direct torque controlled permanent magnet synchronous motor （PMSM） drive. The stator flux was estimated by using the motor voltage model in the stationary frame, and the stator currents were estimated by using the motor current model in the rotor frame. The current estimation errors were then used as feedback signals through a gain matrix. Stator resistance adaptive law was developed based on Lyapunov stability theory. The observer gain matrix was obtained by using the pole placement method. The stability of the adaptive observer was guaranteed by the Lyapunov stability analysis. In addition, a speed controller was designed based on active disturbance rejection control （ADRC） technique to estimate and compensate the load disturbance. Simulation results have confirmed both the effectiveness of the adaptive observer and the anti-load-disturbance performance of the active disturbance rejection controller.     

Adaptive actuator failure compensation and disturbance rejection scheme for spacecraft

An adaptive actuator failure compensation scheme is proposed for attitude tracking control of spacecraft with unknown disturbances and uncertain actuator failures. A new feature of this adaptive control scheme is the adaptation of the failure pattern parameter estimates, as well as the failure signal parameter estimates, for direct adaptive actuator failure compensation. Based on an adaptive backstepping control design, the estimates of the disturbance parameters are used to solve the disturbance rejection problem. The unknown disturbances are compensated completely with the stability of the whole closed-loop system. The scheme is not only able to accommodate uncertain actuator failures, but also robust against unknown external disturbances. Simulation results verify the desired adaptive actuator failure compensation performance.     

视觉导航辅助的自主空中加油建模与仿真

研究了基于视觉导航方式的自主空中加油（AAR）建模问题。分析了影响自主空中加油对接阶段性能的两个最重要因素——相对距离的测量和风扰动,引入了多个摄像机,建立了适合AAR的视觉导航系统模型,建立了大气扰动和尾流等风扰动下的飞行器模型,用三次多项式规划了对接阶段的航迹并设计了LQR航迹跟踪控制律。对接过程仿真表明,视觉导航的估计精度和飞行控制律性能很好地满足了空中加油的要求。

Abstract：

The modeling problem of autonomous aerial refueling based on vision navigation was researched.The two most important factors affecting the performance of AAR were analyzed,which were the measure of the relative distance and wind disturbance.The vision navigation system suitable for AAR was adopted and modeled using multiple cameras.The dynamic model of plane with the effect of wind was built.Path of docking was planed using cubic interpolators and tracking control was designed with LQR.The result of simulation shows that the accuracy of vision navigation system and the performance of control law can meet requires of aerial refueling.     

Parametric approach to track following control of FFSM

A robust task space tracking scheme is proposed for the free-flying space manipulator system.The dynamic equations of the system are derived via the law of momentum conservation,and then a linear state space representation is formulated by local linearization.A parametric approach is applied by using the eigenstructure assignment theory and the model reference method.A feedback stabilizing controller and a feedforward compensation controller are built based on the approach.Then an optimization procedure is followed after that to obtain the desired requirement and characteristics.Simulation results are presented to show the effectiveness of the proposed method.     

Nonlinear autopilot design for interceptors with tail fins and pulse thrusters via θ-D approach

The missile autopilot for an interceptor with tail fins and pulse thrusters is designed via the θ-D approach. The nonlin- ear dynamic model of the pitch and yaw motion of the missile is transformed into a linear-like structure with state-dependent coef- ficient （SDC） matrices. Based on the linear-like structure, a θ-D feedback controller is designed to steer the missile to track refer- ence acceleration commands. A sufficient condition that ensures the asymptotic stability of the tracking system is given based on Lyapunov＇s theorem. Numerical results show that the proposed autopilot achieves good tracking performance and the closed-loop tracking system is asymptotically stable.     

Adaptive Robust Dead-Zone Compensation Control of Electro-Hydraulic Servo Systems with Load Disturbance Rejection

A backstepping method based adaptive robust dead-zone compensation controller is proposed for the electro-hydraulic servo systems(EHSSs) with unknown dead-zone and uncertain system parameters.Variable load is seen as a sum of a constant and a variable part.The constant part is regarded as a parameter of the system to be estimated real time.The variable part together with the friction are seen as disturbance so that a robust term in the controller can be adopted to reject them.Compared with the traditional dead-zone compensation method,a dead-zone compensator is incorporated in the EHSS without constructing a dead-zone inverse.Combining backstepping method,an adaptive robust controller(ARC) with dead-zone compensation is formed.An easy-to-use ARC tuning method is also proposed after a further analysis of the ARC structure.Simulations show that the proposed method has a splendid tracking performance,all the uncertain parameters can be estimated,and the disturbance has been rejected while the dead-zone term is well estimated and compensated.     

QFT control based on zero phase error compensation for flight simulator

To improve the robustness of high-precision servo systems, quantitative feedback theory (QFT) which aims to achieve a desired robust design over a specified region of plant uncertainty is proposed. The robust design problem can be solved using QFT but it fails to guarantee a high precision tracking. This problem is solved by a robust digital QFT control scheme based on zero phase error (ZPE) feed forward compensation. This scheme consists of two parts: a QFT controller in the closed-loop system and a ZPE feed-forward compensator. Digital QFT controller is designed to overcome the uncertainties in the system. Digital ZPE feed forward controller is used to improve the tracking precision. Simulation and real-time examples for flight simulator servo system indicate that this control scheme can guarantee both high robust performance and high position tracking precision.     

Zero phase error control based on neural compensation for flight simulator servo system

1. INTRODUCTION In high precision tracking applications of mechanical systems, feedforward controllers are often used to enhance tracking performance, and they are generally prefilter for the desired trajectory to compensate for the dynamic lag of the closed loop and to extend the tracking bandwidth. Because of the rapid growth of computer technology, digital motion control system has become more and more popular, and feedforward controller design in discrete time domain attracts much atte…     

Dual loop feedback pre-distortion in satellite communication

Since the satellite communication goes in the trend of high-frequency and fast speed, the coefficients updating and the precision of the traditional pre-distortion feedback methods need to be further improved. On this basis, this paper proposes dual loop feedback pre-distortion, which uses two first-order Volterra filter models to reduce the computing complexity and a dynamic error adjustment model to construct a revised feedback to ensure a better pre-distortion performance. The computation complexity, iterative convergence speed and precision of the proposed method are theoretically analyzed. Simulation results show that this dual loop feedback pre-distortion can speed the updating of coefficients and ensure the linearity of the amplifier output.     

Finite-time tracking control for motor servo systems with unknown dead-zones

A finite-time tracking control scheme is proposed in this paper based on the terminal slid- ing mode principle for motor servo systems with unknown nonlinear dead-zone inputs. By using the differential mean value theorem, the dead-zone is represented as a time-varying system and thus the inverse compensation approach is avoided. Then, an indirect terminal sliding mode control （ITSMC） is developed to guarantee the finite-time convergence of the tracking error and to overcome the singu- larity problem in the traditional terminal sliding mode control. In the proposed controller design, the unknown nonlinearity of the system is approximated by a simple sigmoid neural network, and the ap- proximation error is diminished by employing a robust term. Comparative experiments on a turntable servo system are conducted to show the superior performance of the proposed method.     

飞行器自抗扰姿态控制优化与仿真研究

以飞行器姿态控制为背景,设计了俯仰、横侧（解耦）自抗扰控制器。通过扩张观测器的动态补偿获得控制器的鲁棒性。通过被控对象执行机构特性和所希望的闭环性能确定控制器参数的范围。被控对象的状态方程和扩张观测器方程组合在一起,形成扩展状态方程,把控制参数的确定,转化为线性矩阵不等式的求解。仿真结果表明,控制器具有很强的鲁棒性,适应性,快速性和优良的控制品质。

Abstract：

Active Disturbance Rejection Control （ADRC） based pitch attitude and lateral decoupling control were proposed. Robustness was obtained by dynamic compensation of Extended State Observer （ESO）, and the control parameters’ bounds were determined by combination of actuator’s characteristics and specified closed-loop performance. The parameters’ optimization was carried out by LMI approach based on expanded state equations containing the plant and the ESO. The simulation results show that the controller has strong robustness, adaptability and good performance.     

An Application of Optimal Preview Control in Terrain Following System

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飞行仿真转台模糊神经网络补偿的复合控制

针对飞行仿真转台系统的非线性和不确定性,提出了基于模糊神经网络补偿的复合控制器,该控制器由前馈控制器、闭环控制器及模糊神经网络补偿环节组成。前馈环节由零相差跟踪控制器及FIR滤波器构成,闭环控制器由PD控制及干扰观测器构成,补偿环节由一动态模糊神经网络实现,给出了基于Lyapunov函数的稳定性证明。该控制方法突出优点在于兼顾考虑了系统中的结构化不确定性和非结构化不确定性,能够在外部干扰与参数摄动并存的情况下,保证系统的稳定性和跟踪性能。     

Feedforward and feedback optimal control for linear time-varying systems with persistent disturbances

1 .INTRODUCTIONIn nature ,there are various external disturbancesaffecting the performances of systems . Many con-trol problemsinvolve designing a controller capableof stabilizing a given linear system while mini mi-zing the worst-case response to some additive dis-turbances . This problemis relevant to disturbancerejection and cancellation. One application area ofinterest is flight control through wind shear ,where disturbances arise from a modal for windshear based on harmonic oscillati…     

无人直升机自主着舰轨迹跟踪控制

着舰飞行过程中的轨迹跟踪控制能力是影响舰载无人直升机性能的关键因素,针对无人直升机模型不确定性和在飞行时受阵风干扰的问题,基于扩张状态观测器(extend stated observer, ESO)和动态面策略提出一种应用于无人直升机自主着舰的轨迹跟踪控制方法。首先,建立无人直升机数学模型。其次,设计复合扰动ESO,用来观测未建模动态和外界阵风扰动的影响,并采用前馈补偿的方式来抑制系统不确定性,实现系统对扰动的鲁棒性。然后,采用内外环形式的分层结构设计轨迹跟踪控制器,采取动态面策略避免反步法“微分爆炸”和控制参数调整不敏感的问题,并采用Lyapunov方法证明了整个系统是一致渐进稳定的。最后,采用课题组在研直升机进行了仿真实验,仿真结果表明该控制器具有较好的轨迹跟踪性能。     

火电单元机组智能控制系统

提出了一个实现大范围负荷跟踪的火电单元机组智能控制系统．该系统包括设定值调节器、神经网络模糊前馈控制器、模糊反馈控制器和单元机组．设定值调节器根据机组负荷指令提供设定值．前馈控制器采用神经网络模糊控制逼近单元机组的逆稳态特性而得到前馈控制信号，以实现单元机组的大范围运行．反馈控制器则采用模糊控制补偿负荷扰动所引起的单元机组的实际值与设定值的偏差．前馈控制信号与反馈控制信号相加后发出指令到单元机组完成负荷跟踪任务．仿真结果表明，该系统有较好的动态特性，能适应于机组大范围的负荷跟踪．     

一类高精度伺服系统基于模糊神经网络的复合控制

针对高精度伺服系统中存在的各种非线性及不确定性 ,提出了基于模糊神经网络的复合控制方法。控制器由前馈控制器和闭环反馈控制器组成。前馈控制器由零相差跟踪控制器 (ZPETC)及FIR滤波器构成 ,闭环反馈控制器采用模糊神经网络控制 ,包含一个辨识网络FNNI和控制网络FNNC。该控制方法结合了神经网络和模糊推理的优点 ,可以克服各种非线性和不确定性 ,明显提高跟踪性能 ,具有很好的鲁棒性。提出的模糊神经网络结构简单 ,推理算法易于实现 ,并且可以更合理地选择初始权值 ,加快了网络的收敛速度 ,在一定程度上解决了神经网络的实时性问题     

基于粗糙集理论与进化计算的时滞系统Smith控制

Smith预估器是一种有效的大纯滞后补偿控制方法,但对模型的依赖性限制了它在工程实际中的应用。针对被控对象的纯时滞时间的不确定性和系统存在扰动的情形,将基于粗糙集的进化计算与Smith预估器的控制方法相结合,给出了一种在线调整时滞时间和利用前馈进行扰动补偿的自适应控制方法,即通过对反馈误差的在线优化适应性地调整Smith预估器的时滞时间常数和对扰动进行补偿。仿真结果表明了给出方法的有效性。